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空气节流对超燃发动机燃烧性能的影响

邓维鑫 乐嘉陵 王西耀 杨顺华 张弯洲 许明恒

邓维鑫, 乐嘉陵, 王西耀, 杨顺华, 张弯洲, 许明恒. 空气节流对超燃发动机燃烧性能的影响[J]. 航空动力学报, 2013, 28(2): 316-323.
引用本文: 邓维鑫, 乐嘉陵, 王西耀, 杨顺华, 张弯洲, 许明恒. 空气节流对超燃发动机燃烧性能的影响[J]. 航空动力学报, 2013, 28(2): 316-323.
DENG Wei-xin, LE Jia-ling, WANG Xi-yao, YANG Shun-hua, ZHANG Wan-zhou, XU Ming-heng. Air-throttling effect of scramjet combustion characteristics[J]. Journal of Aerospace Power, 2013, 28(2): 316-323.
Citation: DENG Wei-xin, LE Jia-ling, WANG Xi-yao, YANG Shun-hua, ZHANG Wan-zhou, XU Ming-heng. Air-throttling effect of scramjet combustion characteristics[J]. Journal of Aerospace Power, 2013, 28(2): 316-323.

空气节流对超燃发动机燃烧性能的影响

基金项目: 国家自然科学青年科学基金(10902109)

Air-throttling effect of scramjet combustion characteristics

  • 摘要: 为优化隔离段及燃烧室内的流场结构,减小流动速度,提高流道压力,在凹槽稳焰器下游布置空气节流装置,向燃烧室内喷入高压空气,目的是在隔离段建立合适的激波串,以利于点火和火焰稳定.采用CFD方法,对比了无/有空气节流时的冷流流场、燃烧流场,结果表明:节流激波串扩大了低动量区域,激波引起的流动扭曲和较长的驻留时间使得分离流内的空气/燃料混合程度得到显著增强,混合效率由无节流时的40%提高到85%,燃烧效率由无节流时的10%提高到60%.对节流位置和节流量进行了参数化研究,以隔离段入口为坐标原点,分别考察了785,1000,1100mm三个流向节流位置,以及10%,15%,30%三种节流量的影响,结果表明:距离凹槽较近的节流位置对燃烧的影响更为显著,所需节流量更少.30%的节流量将使燃烧室背压急剧提高,引起流动壅塞.研究表明在785mm的流向节流位置采用15%的节流量可获得最好的燃烧性能.

     

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出版历程
  • 收稿日期:  2012-03-14
  • 刊出日期:  2013-02-28

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